AR021476A1 - CANON PERFORATOR CARRIER OF HOLLOW LOADS. - Google Patents
CANON PERFORATOR CARRIER OF HOLLOW LOADS.Info
- Publication number
- AR021476A1 AR021476A1 ARP990104482A ARP990104482A AR021476A1 AR 021476 A1 AR021476 A1 AR 021476A1 AR P990104482 A ARP990104482 A AR P990104482A AR P990104482 A ARP990104482 A AR P990104482A AR 021476 A1 AR021476 A1 AR 021476A1
- Authority
- AR
- Argentina
- Prior art keywords
- hollow
- canon
- charges
- support structure
- carrier
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B3/00—Blasting cartridges, i.e. case and explosive
- F42B3/28—Cartridge cases characterised by the material used, e.g. coatings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
- F42B1/02—Shaped or hollow charges
- F42B1/032—Shaped or hollow charges characterised by the material of the liner
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Forging (AREA)
- Prevention Of Electric Corrosion (AREA)
- Connections Effected By Soldering, Adhesion, Or Permanent Deformation (AREA)
Abstract
Se revela una carga explosiva hueca, con un canon perforador portador y un método para usar dichas cargas explosivas. La carga explosiva cuenta con mayorresistencia a la plastodeformacion para utilizar en un canon perforador,que tiene una banda enes piral alargada abierta al pozo de sondeo en la cual se sujetanlas cargas. La carga hueca es una cápsula de cuerpo hueco y un capuchon de cuerpo hueco, ambos roscados para su fácil acoplamiento. Al menos la cápsula estácompuesta por una aleacionque c ontien entre el 4 y el 12 por ciento por peso de cobre, entre el 2 y el 4 por ciento por peso de aluminio y el resto de zinc eimpurezas. El canon portador consiste en una estructura de sostén alargada con un diámetro apropiado para serintroducido y retirado de un pozo. También estáprovista de aberturas espaciadas que sirven para montaje de las cargas explosivas huecas, conectadas por un cable detonador, y que se fijan mediante medios desujecion a la estructura de sostén. Elmétodo consiste de l os siguientes pasos; sujetar las cargas explosivas huecas a la estructura de sostén segun un patronde perforacion seleccionado; introducir la estructura de sostén con las cargas explosivas huecas dentro de la perforacion; ydetonar las cargas huecas paraperforar por ese medio el pozo.A hollow explosive charge is revealed, with a carrier piercing canon and a method of using such explosive charges. The explosive charge has greater resistance to plastodeformation for use in a piercing canon, which has an elongated pyral band open to the borehole in which the charges are held. The hollow load is a hollow body capsule and a hollow body cap, both threaded for easy coupling. At least the capsule is made up of an alloy that has between 4 and 12 percent by weight of copper, between 2 and 4 percent by weight of aluminum and the rest of zinc and impurities. The carrier canon consists of an elongated support structure with an appropriate diameter to be introduced and removed from a well. It is also provided with spaced openings that are used for mounting hollow explosive charges, connected by a detonator cable, and which are fixed by means of dislocation to the support structure. The method consists of the following steps; fasten the hollow explosive charges to the support structure according to a selected perforation pattern; insert the support structure with the hollow explosive charges into the perforation; and detonate the hollow charges to pierce the well by that means.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/222,442 US6216596B1 (en) | 1998-12-29 | 1998-12-29 | Zinc alloy shaped charge |
Publications (1)
Publication Number | Publication Date |
---|---|
AR021476A1 true AR021476A1 (en) | 2002-07-24 |
Family
ID=22832229
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ARP990104482A AR021476A1 (en) | 1998-12-29 | 1999-09-06 | CANON PERFORATOR CARRIER OF HOLLOW LOADS. |
Country Status (4)
Country | Link |
---|---|
US (1) | US6216596B1 (en) |
AR (1) | AR021476A1 (en) |
AU (1) | AU6237499A (en) |
WO (1) | WO2000039519A2 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10794159B2 (en) | 2018-05-31 | 2020-10-06 | DynaEnergetics Europe GmbH | Bottom-fire perforating drone |
US11408279B2 (en) | 2018-08-21 | 2022-08-09 | DynaEnergetics Europe GmbH | System and method for navigating a wellbore and determining location in a wellbore |
US11661824B2 (en) | 2018-05-31 | 2023-05-30 | DynaEnergetics Europe GmbH | Autonomous perforating drone |
US11834920B2 (en) | 2019-07-19 | 2023-12-05 | DynaEnergetics Europe GmbH | Ballistically actuated wellbore tool |
US12000267B2 (en) | 2021-09-24 | 2024-06-04 | DynaEnergetics Europe GmbH | Communication and location system for an autonomous frack system |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7155049B2 (en) * | 2001-01-11 | 2006-12-26 | Trestle Acquisition Corp. | System for creating microscopic digital montage images |
US20050109501A1 (en) * | 2003-11-26 | 2005-05-26 | Ludwig Wesley N. | Perforating gun with improved carrier strip |
US7533612B1 (en) * | 2004-09-23 | 2009-05-19 | The United States Of America As Represented By The Secretary Of The Army | Projectile height of burst determination method and system |
US8347962B2 (en) | 2005-10-27 | 2013-01-08 | Baker Hughes Incorporated | Non frangible perforating gun system |
US7775279B2 (en) * | 2007-12-17 | 2010-08-17 | Schlumberger Technology Corporation | Debris-free perforating apparatus and technique |
US8342094B2 (en) * | 2009-10-22 | 2013-01-01 | Schlumberger Technology Corporation | Dissolvable material application in perforating |
WO2016037122A1 (en) * | 2014-09-04 | 2016-03-10 | Hunting Titan, Inc. | Zinc one piece link system |
WO2016161376A1 (en) * | 2015-04-02 | 2016-10-06 | Hunting Titan, Inc. | Snap-on liner retention device |
BR112020005090A2 (en) | 2017-09-14 | 2020-09-15 | DynaEnergetics Europe GmbH | directed jet explosive charge liner, directed jet explosive charge liner and method for drilling a well bore |
BR112020009904A2 (en) | 2017-11-29 | 2020-10-13 | DynaEnergetics Europe GmbH | molded load closure element, molded load with encapsulated slot and exposed drill barrel system |
US11480038B2 (en) | 2019-12-17 | 2022-10-25 | DynaEnergetics Europe GmbH | Modular perforating gun system |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2632394B1 (en) | 1986-07-24 | 1990-11-30 | France Etat Armement | EXPLOSIVE LOAD GENERATOR OF CORE |
US4885993A (en) * | 1988-02-17 | 1989-12-12 | Goex, Inc. | Shaped charge with bifurcated projection for detonating cord |
US4875413A (en) * | 1988-11-30 | 1989-10-24 | Jet Research Center, Inc. | Apparatus for perforating wells |
US5078054A (en) * | 1989-03-14 | 1992-01-07 | Olin Corporation | Frangible projectile |
US4990310A (en) | 1989-09-11 | 1991-02-05 | General Motors Corporation | Creep-resistant die cast zinc alloys |
US4958569B1 (en) | 1990-03-26 | 1997-11-04 | Olin Corp | Wrought copper alloy-shaped charge liner |
US5098487A (en) | 1990-11-28 | 1992-03-24 | Olin Corporation | Copper alloys for shaped charge liners |
AU2951995A (en) * | 1994-07-06 | 1996-01-25 | Lockheed Martin Energy Systems, Inc. | Non-lead, environmentally safe projectiles and method of making same |
US5509728A (en) | 1994-12-14 | 1996-04-23 | General Motors Corporation | Brake system zinc-base alloy components |
WO1996023193A1 (en) * | 1995-01-26 | 1996-08-01 | Federal-Hoffman, Inc., Doing Business As Federal Cartridge Co. | Non-toxic bullet |
US5656791A (en) | 1995-05-15 | 1997-08-12 | Western Atlas International, Inc. | Tungsten enhanced liner for a shaped charge |
US5679920A (en) * | 1995-08-03 | 1997-10-21 | Federal Hoffman, Inc. | Non-toxic frangible bullet |
US5648635A (en) * | 1995-08-22 | 1997-07-15 | Lussier; Norman Gerald | Expendalble charge case holder |
-
1998
- 1998-12-29 US US09/222,442 patent/US6216596B1/en not_active Expired - Fee Related
-
1999
- 1999-05-19 WO PCT/US1999/010983 patent/WO2000039519A2/en active Application Filing
- 1999-05-19 AU AU62374/99A patent/AU6237499A/en not_active Abandoned
- 1999-09-06 AR ARP990104482A patent/AR021476A1/en active IP Right Grant
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10794159B2 (en) | 2018-05-31 | 2020-10-06 | DynaEnergetics Europe GmbH | Bottom-fire perforating drone |
US11661824B2 (en) | 2018-05-31 | 2023-05-30 | DynaEnergetics Europe GmbH | Autonomous perforating drone |
US11408279B2 (en) | 2018-08-21 | 2022-08-09 | DynaEnergetics Europe GmbH | System and method for navigating a wellbore and determining location in a wellbore |
US11834920B2 (en) | 2019-07-19 | 2023-12-05 | DynaEnergetics Europe GmbH | Ballistically actuated wellbore tool |
US12000267B2 (en) | 2021-09-24 | 2024-06-04 | DynaEnergetics Europe GmbH | Communication and location system for an autonomous frack system |
Also Published As
Publication number | Publication date |
---|---|
AU6237499A (en) | 2000-07-31 |
US6216596B1 (en) | 2001-04-17 |
WO2000039519A3 (en) | 2000-10-19 |
WO2000039519A2 (en) | 2000-07-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG | Grant, registration |